296.0 Aluminum vs. EN 1.4419 Stainless Steel
296.0 aluminum belongs to the aluminum alloys classification, while EN 1.4419 stainless steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.
For each property being compared, the top bar is 296.0 aluminum and the bottom bar is EN 1.4419 stainless steel.
Metric UnitsUS Customary Units
Mechanical Properties
| Elastic (Young's, Tensile) Modulus, GPa | 72 | |
| 200 |
| Elongation at Break, % | 3.2 to 7.1 | |
| 11 to 17 |
| Fatigue Strength, MPa | 47 to 70 | |
| 230 to 680 |
| Poisson's Ratio | 0.33 | |
| 0.28 |
| Shear Modulus, GPa | 27 | |
| 76 |
| Tensile Strength: Ultimate (UTS), MPa | 260 to 270 | |
| 660 to 1590 |
| Tensile Strength: Yield (Proof), MPa | 120 to 180 | |
| 370 to 1240 |
Thermal Properties
| Latent Heat of Fusion, J/g | 420 | |
| 280 |
| Maximum Temperature: Mechanical, °C | 170 | |
| 790 |
| Melting Completion (Liquidus), °C | 630 | |
| 1440 |
| Melting Onset (Solidus), °C | 540 | |
| 1400 |
| Specific Heat Capacity, J/kg-K | 870 | |
| 480 |
| Thermal Conductivity, W/m-K | 130 to 150 | |
| 30 |
| Thermal Expansion, µm/m-K | 22 | |
| 11 |
Electrical Properties
| Electrical Conductivity: Equal Volume, % IACS | 33 to 37 | |
| 2.8 |
| Electrical Conductivity: Equal Weight (Specific), % IACS | 99 to 110 | |
| 3.2 |
Otherwise Unclassified Properties
| Base Metal Price, % relative | 11 | |
| 8.0 |
| Density, g/cm3 | 3.0 | |
| 7.7 |
| Embodied Carbon, kg CO2/kg material | 7.8 | |
| 2.2 |
| Embodied Energy, MJ/kg | 150 | |
| 30 |
| Embodied Water, L/kg | 1110 | |
| 110 |
Common Calculations
| Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 7.6 to 15 | |
| 95 to 170 |
| Resilience: Unit (Modulus of Resilience), kJ/m3 | 110 to 220 | |
| 350 to 3920 |
| Stiffness to Weight: Axial, points | 13 | |
| 14 |
| Stiffness to Weight: Bending, points | 46 | |
| 25 |
| Strength to Weight: Axial, points | 24 to 25 | |
| 24 to 57 |
| Strength to Weight: Bending, points | 30 to 31 | |
| 22 to 39 |
| Thermal Diffusivity, mm2/s | 51 to 56 | |
| 8.1 |
| Thermal Shock Resistance, points | 12 | |
| 23 to 55 |
Alloy Composition
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| Aluminum (Al), % | 89 to 94 | |
| 0 |
| Carbon (C), % | 0 | |
| 0.36 to 0.42 |
| Chromium (Cr), % | 0 | |
| 13 to 14.5 |
| Copper (Cu), % | 4.0 to 5.0 | |
| 0 |
| Iron (Fe), % | 0 to 1.2 | |
| 82 to 86 |
| Magnesium (Mg), % | 0 to 0.050 | |
| 0 |
| Manganese (Mn), % | 0 to 0.35 | |
| 0 to 1.0 |
| Molybdenum (Mo), % | 0 | |
| 0.6 to 1.0 |
| Nickel (Ni), % | 0 to 0.35 | |
| 0 |
| Phosphorus (P), % | 0 | |
| 0 to 0.040 |
| Silicon (Si), % | 2.0 to 3.0 | |
| 0 to 1.0 |
| Sulfur (S), % | 0 | |
| 0 to 0.015 |
| Titanium (Ti), % | 0 to 0.25 | |
| 0 |
| Zinc (Zn), % | 0 to 0.5 | |
| 0 |
| Residuals, % | 0 to 0.35 | |
| 0 |